CN109552617A - A kind of unmanned plane propeller adjustment - Google Patents
A kind of unmanned plane propeller adjustment Download PDFInfo
- Publication number
- CN109552617A CN109552617A CN201811447061.7A CN201811447061A CN109552617A CN 109552617 A CN109552617 A CN 109552617A CN 201811447061 A CN201811447061 A CN 201811447061A CN 109552617 A CN109552617 A CN 109552617A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- main body
- motor
- fuselage main
- rod
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention discloses a kind of unmanned plane propeller adjustment, including fuselage main body, the wing bar being at right angles arranged there are four being set in fuselage main body, the upper surface of wing bar is equipped with groove one, rod set is equipped in groove one and at fuselage main body center, rod set interpolation is equipped with rod piece, it is equipped between rod piece and rod set and is used for spring connecting the two, the other end of rod piece is equipped with motor, the transmission shaft of motor is equipped with flabellum, set is equipped with baffle on motor, and the two sides of wing bar are equipped with the gear tooth for limiting baffle.Advantages of the present invention: i.e. the position of propeller is adjustable, thus the flying height and posture of changeable unmanned plane.
Description
Technical field
The present invention relates to a kind of regulating device, specifically a kind of unmanned plane propeller adjustment.
Background technique
Unmanned plane, has become the object for playing a kind of hobby of model plane people now, and the propeller of existing unmanned plane is substantially
Fixed, adjustment appropriate can not be carried out, therefore be unable to satisfy requirement of the player to unmanned plane during flying posture etc., the scope of application
It is small.
Summary of the invention
In view of the above existing problems in the prior art, the present invention provides a kind of unmanned plane propeller adjustments, can
Position of the propeller apart from fuselage main body is adjusted, to provide more flight attitudes and height, to meet the needs of user, is fitted
It is wider with range.
To achieve the goals above, a kind of unmanned plane propeller adjustment that the present invention uses, including fuselage main body,
It is set in the fuselage main body there are four the wing bar being at right angles arranged, the upper surface of described wing bar is equipped with groove one, described
Groove one in and be equipped with rod set at the fuselage main body center, the rod set interpolation is equipped with rod piece, the rod piece with
It is equipped between rod set and is used for spring connecting the two, the other end of the rod piece is equipped with motor, the transmission shaft of the motor
It is equipped with flabellum, set is equipped with baffle on the motor, and the two sides of the wing bar are equipped with for limiting baffle
Keep off tooth.
The gear tooth is equipped with several groups.
The thickness of the baffle is less than the length of motor transmission shaft.
In the use of the present invention, adjustable position of the propeller apart from fuselage main body, come provide more flight attitudes and
Highly, meets the needs of user, the scope of application is wider.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of unmanned plane propeller adjustment of the present invention；
In figure: 1, fuselage main body, 2, wing bar, 3, groove, 4, rod set, 5, rod piece, 6, spring, 7, motor, 8, flabellum, 9, gear
Plate, 10, gear tooth.
Specific embodiment
It is right below by attached drawing and embodiment to keep purpose of the present invention technical solution and advantage more clear
The present invention is further elaborated.However, it should be understood that specific embodiment described herein is only used to explain this hair
Range that is bright, being not intended to restrict the invention.
As shown in Figure 1, a kind of unmanned plane propeller adjustment that the present invention uses, including fuselage main body 1, it is described
It is set in fuselage main body 1 there are four the wing bar 2 being at right angles arranged, the upper surface of described wing bar 2 is equipped with groove 1, described
Rod set 4 is equipped in groove 1 and at 1 center of fuselage main body, 4 interpolation of rod set is equipped with rod piece 5, the rod piece
It is equipped between 5 and rod set 4 and is used for spring 6 connecting the two, the other end of the rod piece 5 is equipped with motor 7, the motor 7
Transmission shaft be equipped with flabellum 8, set is equipped with baffle 9 on the motor 7, and the two sides of the wing bar 2, which are equipped with, to be used
In the gear tooth 10 of limitation baffle 9.
The gear tooth 10 is equipped with several groups.
The thickness of the baffle 9 is less than the length of 7 transmission shaft of motor.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modification, equivalent replacement or improvement etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (3)
1. a kind of unmanned plane propeller adjustment, including fuselage main body (1), set in the fuselage main body (1) there are four
The wing bar (2) being at right angles arranged, it is characterised in that: the upper surface of described wing bar (2) is equipped with groove one (3), and described is recessed
Rod set (4) are equipped in slot one (3) and at fuselage main body (1) center, the rod set (4) interpolation is equipped with rod piece (5), institute
It is equipped between the rod piece (5) stated and rod set (4) and is used for spring connecting the two (6), the other end of the rod piece (5) is equipped with electricity
The transmission shaft of machine (7), the motor (7) is equipped with flabellum (8), covers and is equipped with baffle (9) on the motor (7), described
The two sides of wing bar (2) be equipped with gear tooth (10) for limiting baffle (9).
2. a kind of unmanned plane propeller adjustment according to claim 1, it is characterised in that: the gear tooth (10)
Equipped with several groups.
3. a kind of unmanned plane propeller adjustment according to claim 1, it is characterised in that: the baffle (9)
Thickness be less than motor (7) transmission shaft length.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811447061.7A CN109552617A (en) | 2018-11-29 | 2018-11-29 | A kind of unmanned plane propeller adjustment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811447061.7A CN109552617A (en) | 2018-11-29 | 2018-11-29 | A kind of unmanned plane propeller adjustment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109552617A true CN109552617A (en) | 2019-04-02 |
Family
ID=65868107
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811447061.7A Pending CN109552617A (en) | 2018-11-29 | 2018-11-29 | A kind of unmanned plane propeller adjustment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109552617A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077587A (en) * | 2019-04-30 | 2019-08-02 | 中北大学 | A kind of displacement aircraft and its control method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB338632A (en) * | 1928-12-05 | 1930-11-27 | Walter Villa Gilbert | |
| CN205010472U (en) * | 2015-09-01 | 2016-02-03 | 湖南云顶智能科技有限公司 | A scalable horn for unmanned aerial vehicle |
| CN106394887A (en) * | 2016-10-24 | 2017-02-15 | 杭州鼎曜信息技术有限公司 | Multi-rotor-wing unmanned aerial vehicle and control method thereof |
| CN107458586A (en) * | 2016-06-03 | 2017-12-12 | 上海九鹰电子科技有限公司 | Multi-rotor aerocraft and telescoping member |
| CN107878745A (en) * | 2017-12-18 | 2018-04-06 | 南京灿华光电设备有限公司 | It is a kind of to be easy to folded unmanned plane |
| CN207328802U (en) * | 2017-08-30 | 2018-05-08 | 普宙飞行器科技（深圳）有限公司 | A kind of telescopic unmanned vehicle |
-
2018
- 2018-11-29 CN CN201811447061.7A patent/CN109552617A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB338632A (en) * | 1928-12-05 | 1930-11-27 | Walter Villa Gilbert | |
| CN205010472U (en) * | 2015-09-01 | 2016-02-03 | 湖南云顶智能科技有限公司 | A scalable horn for unmanned aerial vehicle |
| CN107458586A (en) * | 2016-06-03 | 2017-12-12 | 上海九鹰电子科技有限公司 | Multi-rotor aerocraft and telescoping member |
| CN106394887A (en) * | 2016-10-24 | 2017-02-15 | 杭州鼎曜信息技术有限公司 | Multi-rotor-wing unmanned aerial vehicle and control method thereof |
| CN207328802U (en) * | 2017-08-30 | 2018-05-08 | 普宙飞行器科技（深圳）有限公司 | A kind of telescopic unmanned vehicle |
| CN107878745A (en) * | 2017-12-18 | 2018-04-06 | 南京灿华光电设备有限公司 | It is a kind of to be easy to folded unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110077587A (en) * | 2019-04-30 | 2019-08-02 | 中北大学 | A kind of displacement aircraft and its control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190402 |
|
| WD01 | Invention patent application deemed withdrawn after publication |